Non-ferrous Flashcards
What are the advantages of titanium
Strong Light weigh Strength to weight ratio Heat resistance Corrosion resistance
What are the disvantages of titanium
Dust ignites
Need to cut with sharp tools
Colbolt still
What is titanium used for
Cooler section of gas turbine engines
Advances of aluminium
3 times light than steel
Produced in cast form
Corrosion resistance
Disadvantages of aluminium
Course grain structure
Brittle
Too malleable
What is the 1st digit in aluminium alloy
Majority alloying element
What is the 2nd digit in aluminium alloy
Any modification
What is the last 2 digits in aluminium alloy
Any other alloying elements
What alloying element are not heat treatable
Copper and zinc
What is 1
Aluminium
What is 2
Copper
What is 3
Manganese
What is 4
Silicon
What is number 5
Magnesium
What is 6
Magnesium and silicon
What is 7
Zinc
What is 8
Tin
What is work hardening
known as strain hardening or cold working, is the strengthening of a metal by plastic deformation
Used for non heat treatable aluminium alloys
Annealing
procedure for aluminium alloys consists of heating the alloys to an elevated temperature, holding or soaking them at this temperature for a length of time
Then cooled slowly
Leaves in condition for cold working
Solution heat treatment
heated in either a molten sodium or potassium nitrate bath or in a hot-air furnace. The temperature is then held to within plus or minus 50°C, long enough for the copper to be taken into the solid solution with the aluminium matrix
Metal removed and quenched with 10 seconds
Cold working
will cause the copper to precipitate at grain boundaries and harden the alloy.
Natural age Harding
willoccuratroomtemperatureandistheprocess by which the copper precipitates at the grain boundaries, this hardens the aluminium to full strength over a period of several days.
Artificial ageing or precipitation hardening
temperature is raised to between 1200C and 1900C, depending on alloying element, this increases the precipitation hardening process and also raises the final strength of the alloy
What has no quench
Annealing
F
As fabricated
I
Annealing
H
Strain hardening
W
Solution heat treated
T
Heat-treated to produce stable tempers other than F, O, or H
T3
Solution heat-treated and cold worked.
T4
Solution heat-treated and naturally aged
T2
Annealed
T6
Solution heat-treated and artificially aged.
Magnesium properties
Highly susceptible to corrosion
Difficult to work with
Highly flammable
What fire extinguisher to use in magnesium
Dry powder
Helium
Argon
Sand
Glare
Glass reinforced laminate
thin layers of metal sheet and uni-directional fibre layers embedded in an adhesive system. Glare is an optimised FML for aircraft and consists of alternating layers of aluminium and glass fibre pregreg layers.
Advantage of glare
- High strength
- Fatigue resistant
- Damage tolerant
- Impact and blast resistant
- Fire resistant
- Thermal isolation
Where is glare used
Blast resistance cointainer
Cargo floors and liners
Leading edges